Path: SC/Ephem
% Compute total change in longitude between two orbits. Computes the change in longitude accounting for multiple revolutions in between the first and second values based on the mean motion. Since version 1. -------------------------------------------------------------------------- Form: dL = DeltaML( L1, L2, t1, t2, n ) -------------------------------------------------------------------------- ------ Inputs ------ L1 (1,:) Initial Longitude (deg) L2 (1,:) Final Longitude (deg) t1 (1,:) Initial Time (days) t2 (1,:) Final Time (days) n (1,:) Daily motion (deg/day) ------- Outputs ------- dL (1,:) Change in longitude (deg) --------------------------------------------------------------------------
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